Euler calculations for wings using Cartesian grids
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-356
Reference24 articles.
1. Lasinski, T. A. Andrew. A. E. Sorenson. R. L., Chaussec. D. S., Pulliam, T. H. and Kutler, P. "Computation of the Steady Viscous Plow Over e Tri-Element 'Augmenter Wing Airfoil' ,"AIM Paper 82-0021, January 1982.
2. Atta, It. H. and Vadyak. T. "A Grid Interfacing Zonal AlRorithm for Three Dimensional Transonic Flow 8 About Aircraft Confimratione: A I M Paper 82-1017, June 1982.
3. Jameson, A., Baker, T. J. and Weatherill, N. P. "Calculation of Inviscid Transonic Plow Over a mmplex Aircraft ,"AIM Paper 86-0103, January 1986.
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